[1] 中国航空报社. 中俄远程宽体客机模型首次展示[EB/OL].北京:中国航空报社, 2016. (2016-12-29)[2016-12-29]. http://www.cannews.com.cn/epaper/zghkb/2016/12/29/A02/story/1289549.shtml. China Aviation News. First exhibition of China-Russia LRWB aircraft model[EB/OL].Beijing: China Aviation News, 2016. (2016-12-29)[2016-12-29]. http://www.cannews.com.cn/epaper/zghkb/2016/12/29/A02/story/1289549.shtml (in Chinese).
[2] JASON H. Advances in hydraulics and actuators[J]. Aircraft Technology, 2014, 95: 20-27.
[3] STEFAN F. Electro-hydrostatic actuators for aircraft primary flight control—Types, modeling and evaluation[C]//5th Scandinavian International Conference on Fluid Power, 1997: 1-16.
[4] 多米尼克·冯·博斯施, 张魏. "多电"控制舵面作动器——下一代运输机的一个方案[J]. 电力电子, 2006(4): 15-18. DOMINIQUE V B, ZHANG W. "More electric" control surface actuator, a standard for the next generation of transport aircraft[J]. Power Electronics, 2006(4):15-18 (in Chinese).
[5] EATON'S Aerospace. Airbus A380 system overview: Eaton's aerospace product capabilities:C5-37A[R]. Eaton: Eaton's Aerospace, 2006.
[6] DOMINIQUE V B, NAUCK B. "More electric" control surface actuation, a standard for the next generation of transport aircraft[J]. Power Electronics, 2006, 41: 637-651.
[7] ALLE R B. Liebherr aerospace participation in the A380[R]. Kirchdorf: Libeherr Aerospace, 2003.
[8] AMIT K R. Electric actuation for flight & engine control: Evolution & challenges: SAE-ACGSC Mtg99[R]. Boulder: Hispano-Suiza SAFRAN Group, 2007.
[9] DOMINIQUE V B. The A380 flight control electro hydrostatic actuators, achievements and lessons learnt[C]//25th International Congress of the Aeronautical Sciences, 2006.
[10] PHILIP B H. All-electric aircraft research speeds up[J]. Aerospace America, 2009: 4-7.
[11] 程不时, 李云军, 王智宇. 飞机设计手册——民用飞机总体设计[M]. 北京: 航空工业出版社, 2003: 446-478, 537-553. CHENG B S, LI Y J, WANG Z Y. Aircraft design manual—Civil aircraft design[M]. Beijing: Aviation Industry Press, 2003: 446-478, 537-553 (in Chinese).
[12] XAVIER L. A380 flight control overview[R]. Hamburg: Airbus Flight Control, 2007.
[13] 冯斌. 波音787的新技术[J].航空维修与工程, 2005(5):37-39. FENG B. New technology of Boeing 787[J].Aviation Maintenance & Engineering, 2005(5):37-39 (in Chinese).
[14] ILAN B. All/more electric aircraft engine & airframe systems implementation[C]//The 9th Israeli Symposium on Jet Engines and Gas Turbines, 2010: 32-37.
[15] KAMIAR J K. Future aircraft power systems-integration challenges[R]. Chicago: Boeing Company, 2007.
[16] MOOG Aircraft Group. World leader in flight control systems and critical control applications: 500-1740708[R]. New York: MOOG Aircraft Group, 2008.
[17] IAN M, ALLAN S. Aircraft systems mechanical, electrical, and avionics subsystems integration[M]. Hoboken: Wiley, 2001: 182-192.
[18] CRAIG P L, JAMES M P. Thermal management of electromechanical actuation on an all-electric aircraft[C]//26th International Congress of the Aeronautical Sciences, 2008: 5-8.
[19] JERRY L, STEPHEN S. Electro hydrostatic actuators for control of undersea vehicles: NOIA6240[C]//Joint Undersea Warfare Technology Fall Conference, 2006.
[20] ROBERT N. Performance of an electro-hydrostatic actuator on the F-18 systems: NASA/TM-97-206224[R]. Washington, D.C.: NASA, 1997.
[21] MENG F L. Actuation system design with electrically powered actuators[D]. Cranfield: Cranfield University, 2011: 46-54.
[22] MICHEL T. EMAs for flight controls actuation system—An important step achieved in 2011:2011-01-2732 [R]. New York: SAE International, 2011.
[23] OLIVIER L, ETIENNE F, XAVIER R. EEA 2004 from the more electric aircraft to the all electric aircraft: State of the art & prospective: X24PR0401420[R]. London: EEA 2004-EYAE, 2004. |